Model airplane double-vertical-fin airplane linkage structure

Abstract

The utility model discloses a model airplane double vertical fin airplane linkage structure which comprises a lead screw steering engine, a vertical fin rocker arm, a third carbon rod and a front wheel, one end of the third carbon rod is connected with a first linkage steel wire through a first connecting piece, and the other end of the third carbon rod is connected with a second linkage steel wire through a second connecting piece. The first linkage steel wire is provided with a first vertical fin rudder surface support, and the second linkage steel wire is provided with a second vertical fin rudder surface support. The lead screw steering engine drives the first carbon rod and the rear connecting steel wire to move in a reciprocating mode, the rear connecting steel wire is connected with the vertical fin rocker arm, and the middle connecting piece is installed in the middle of the third carbon rod and connected with the vertical fin rocker arm through the second carbon rod. The front wheel is provided with a front wheel steel wire, the front wheel steel wire is provided with a front wheel rotating shaft, the front wheel rotating shaft is provided with a front wheel rocker arm, and the front wheel rocker arm is connected with the first carbon rod through a front connecting steel wire. The device is simple in structure and can achieve the effect of simultaneous linkage of the double vertical fins and the front wheel.

Description

Technical Field

[0001] This utility model relates to the field of model aircraft technology, specifically a linkage structure for a twin-tail model aircraft. Background Technology

[0002] Model aircraft, as the name suggests, are model airplanes built to resemble actual aircraft. They are non-manned aircraft designed for recreational use. Model aircraft have transcended the narrow scope of research for aerospace scientists, becoming a learning and recreational tool for aerospace and aviation enthusiasts. In model aircraft, steering during flight is controlled by rotating the vertical stabilizer, while steering during taxiing is controlled by rotating the tailwheel. Typically, servos are installed on the fuselage to control the vertical stabilizer and tailwheel rotation, respectively.

[0003] The existing announcement number CN217745716U discloses a linkage structure for model aircraft, used to control the left and right swinging of the vertical tail and tail wheel, including a vertical tail swing arm, a drive assembly, a vertical tail connector, and a tail wheel assembly. The vertical tail swing arm is rotatably connected to the fuselage. The drive assembly is mounted on the fuselage, and its output end is connected to the vertical tail swing arm to drive the vertical tail swing arm to rotate. The vertical tail connector is connected to both the vertical tail swing arm and the vertical tail, and is used to drive the rear-driven vertical tail to swing left and right by the vertical tail swing arm. The tail wheel assembly is connected to both the vertical tail swing arm and the tail wheel, and is used to drive the rear-driven tail wheel to swing left and right by the vertical tail swing arm. The drive assembly drives the vertical tail swing arm to rotate, and the rotation of the vertical tail swing arm drives the vertical tail to swing through the vertical tail connector, and drives the tail wheel to swing through the tail wheel assembly; the swinging of the vertical tail and tail wheel is controlled simultaneously by a single drive assembly.

[0004] While existing technologies have achieved linkage of the vertical tails, they cannot achieve control of the twin vertical tails and cannot be linked simultaneously with the front wheel. Therefore, we propose a linkage structure for a model aircraft with twin vertical tails. Utility Model Content

[0005] The purpose of this invention is to provide a linkage structure for a twin-tail model aircraft to solve the problems in the prior art.

[0006] To achieve the above objectives, this utility model provides the following technical solution: a linkage structure for a model aircraft with twin vertical tails, including a lead screw servo, a vertical tail rocker arm, a third carbon rod, and a front wheel. One end of the third carbon rod is connected to a first linkage wire via a first connector, and the other end of the third carbon rod is connected to a second linkage wire via a second connector. A first vertical tail control surface bracket is installed on the first linkage wire, and a second vertical tail control surface bracket is installed on the second linkage wire.

[0007] The lead screw servo drives the first carbon rod and the rear connecting wire to reciprocate. The rear connecting wire is connected to the vertical tail rocker arm. An intermediate connecting piece is installed in the middle of the third carbon rod. The intermediate connecting piece is connected to the vertical tail rocker arm through the second carbon rod.

[0008] The front wheel is equipped with a front wheel spoke, the front wheel spoke is equipped with a front wheel axle, the front wheel axle is equipped with a front wheel rocker arm, and the front wheel rocker arm is connected to the first carbon rod via a front connecting wire.

[0009] Preferably, a front wheel axle sleeve is fitted on the outer side of the front wheel axle, and the front wheel rocker arm and the front wheel axle are fixed together by front screws.

[0010] Preferably, it also includes a fixing base, on which the tail rocker arm is fitted, and a rear screw for limiting the position of the tail rocker arm is installed on the top of the fixing base.

[0011] Preferably, the vertical tail rocker arm has an L-shaped structure.

[0012] Preferably, the first vertical tail rudder surface bracket is equipped with a first vertical tail, and the second vertical tail rudder surface bracket is equipped with a second vertical tail.

[0013] Compared with the prior art, the beneficial effects of this utility model are: by driving the twin vertical tails through the lead screw servo motor, the rear connecting steel wire, the vertical tail rocker arm, the intermediate connecting part, the third carbon rod, the connecting part, the linkage steel wire, and the vertical tail control surface bracket, the twin vertical tails are moved. At the same time, the nose wheel rocker arm is driven by the steel wire through the mounting hole on the vertical tail rocker arm, so that the nose wheel moves together with the twin vertical tails, achieving the effect of aircraft linkage. The structure of this application is simple and can achieve the effect of simultaneous linkage of the twin vertical tails and the nose wheel. Attached Figure Description

[0014] The accompanying drawings are provided to further illustrate the present invention and form part of the specification. They are used together with the embodiments of the present invention to explain the present invention, but do not constitute a limitation thereof. In the drawings:

[0015] Figure 1 This is a schematic diagram of the structure of this utility model;

[0016] Figure 2 This is a utility model Figure 1 Exploded view;

[0017] Figure 3 This is a schematic diagram of the structure of this utility model in use;

[0018] Figure 4 This is a utility model Figure 1 A partial structural diagram at the right end;

[0019] Figure 5 This is a utility model Figure 1 A schematic diagram of the partial structure on the left.

[0020] In the diagram: 1. Front wheel; 2. Front wheel spokes; 3. Front wheel axle; 4. Front wheel axle sleeve; 5. Front connecting wire; 6. Front bolt; 7. Front wheel rocker arm; 8. First carbon rod; 9. Lead screw servo; 10. Rear connecting wire; 11. Vertical tail rocker arm; 12. Rear bolt; 13. Mounting base; 14. Second carbon rod; 15. Intermediate connector; 16. Third carbon rod; 17. First connector; 18. First linkage wire; 19. First vertical tail rudder surface bracket; 20. Second connector; 21. Second linkage wire; 22. Second vertical tail rudder surface bracket; 23. First vertical tail; 24. Second vertical tail. Detailed Implementation

[0021] To make the objectives, technical solutions, and advantages of the embodiments of this utility model clearer, the technical solutions of the embodiments of this utility model will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some, not all, of the embodiments of this utility model. Based on the embodiments of this utility model, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of this utility model. Therefore, the following detailed description of the embodiments of this utility model provided in the accompanying drawings is not intended to limit the scope of the claimed utility model, but merely to represent selected embodiments of this utility model.

[0022] Please see Figure 1-5 In this embodiment of the utility model, a linkage structure for a model aircraft with twin vertical tails includes a screw servo 9, a vertical tail rocker arm 11, a third carbon rod 16, and a front wheel 1. One end of the third carbon rod 16 is connected to a first linkage wire 18 via a first connector 17, and the other end of the third carbon rod 16 is connected to a second linkage wire 21 via a second connector 20. A first vertical tail control surface bracket 19 is mounted on the first linkage wire 18, and a second vertical tail control surface bracket 22 is mounted on the second linkage wire 21. A first vertical tail 23 is mounted on the first vertical tail control surface bracket 19, and a second vertical tail 24 is mounted on the second vertical tail control surface bracket 22. The screw servo 9 pushes the rear connecting wire, the vertical tail rocker arm, the intermediate connector, the third carbon rod, the connector, the linkage wire, and the vertical tail control surface bracket to drive the twin vertical tails. At the same time, the front wheel rocker arm is pushed by a wire through the mounting hole on the vertical tail rocker arm, so that the front wheel moves together with the twin vertical tails, achieving the effect of aircraft linkage.

[0023] The lead screw servo motor 9 drives the first carbon rod 8 and the rear connecting steel wire 10 to reciprocate. The rear connecting steel wire 10 is connected to the vertical tail rocker arm 11. The middle part of the third carbon rod 16 is equipped with an intermediate connecting piece 15. The intermediate connecting piece 15 is connected to the vertical tail rocker arm 11 through the second carbon rod 14. The vertical tail rocker arm 11 has an L-shaped structure. The vertical tail rocker arm 11 is sleeved on the fixed base 13. The top of the fixed base 13 is equipped with a rear screw 1 that limits the vertical tail rocker arm 11.

[0024] The front wheel 1 is equipped with a front wheel wire 2, the front wheel wire 2 is equipped with a front wheel axle 3, the front wheel axle 3 is equipped with a front wheel rocker arm 7, the front wheel rocker arm 7 is connected to the first carbon rod 8 through a front connecting wire 5; a front wheel axle sleeve 4 is fitted on the outside of the front wheel axle 3, and the front wheel rocker arm 7 and the front wheel axle 3 are fixed together by a front screw 6.

[0025] The working principle of this utility model is as follows: the screw servo motor 9 pushes the rear connecting steel wire, the vertical tail rocker arm, the intermediate connecting part, the third carbon rod, the connecting part, the linkage steel wire, and the vertical tail control surface bracket to drive the movement of the two vertical tails. At the same time, the steel wire pushes the front wheel rocker arm through the hanging hole on the vertical tail rocker arm so that the front wheel moves together with the two vertical tails, achieving the effect of aircraft linkage.

[0026] Finally, it should be noted that the above description is merely a preferred embodiment of this utility model and is not intended to limit the utility model. Although the utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of this utility model should be included within the protection scope of this utility model.

Claims

1. A linkage structure for a twin-tail model aircraft, comprising a lead screw servo (9), a tail rocker arm (11), a third carbon rod (16), and a nose wheel (1), characterized in that: One end of the third carbon rod (16) is connected to the first linkage wire (18) through the first connector (17), and the other end of the third carbon rod (16) is connected to the second linkage wire (21) through the second connector (20). The first linkage wire (18) is equipped with a first vertical tail rudder surface bracket (19), and the second linkage wire (21) is equipped with a second vertical tail rudder surface bracket (22). The lead screw servo (9) drives the first carbon rod (8) and the rear connecting wire (10) to reciprocate. The rear connecting wire (10) is connected to the vertical tail rocker arm (11). The middle part of the third carbon rod (16) is equipped with an intermediate connector (15). The intermediate connector (15) is connected to the vertical tail rocker arm (11) through the second carbon rod (14). The front wheel (1) is equipped with a front wheel wire (2), the front wheel wire (2) is equipped with a front wheel axle (3), the front wheel axle (3) is equipped with a front wheel rocker arm (7), and the front wheel rocker arm (7) is connected to the first carbon rod (8) through a front connecting wire (5).

2. The linkage structure for a twin-tail model aircraft according to claim 1, characterized in that: The front wheel axle (3) is fitted with a front wheel axle sleeve (4), and the front wheel rocker arm (7) and the front wheel axle (3) are fixed together by a front screw (6).

3. The linkage structure for a twin-tail model aircraft according to claim 1, characterized in that: It also includes a fixed base (13), on which the vertical tail rocker arm (11) is fitted, and a rear screw (12) for limiting the vertical tail rocker arm (11) is installed on the top of the fixed base (13).

4. The linkage structure for a twin-tail model aircraft according to claim 1, characterized in that: The vertical tail rocker arm (11) has an L-shaped structure.

5. The linkage structure for a twin-tail model aircraft according to claim 1, characterized in that: The first vertical tail rudder surface bracket (19) is equipped with a first vertical tail (23), and the second vertical tail rudder surface bracket (22) is equipped with a second vertical tail (24).

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